DocumentCode :
1704092
Title :
Failure propagation analysis of aircraft engine system based on the small-world net model
Author :
Liu Xiaofeng ; An Siqi
Author_Institution :
Sch. of Transp. Sci. & Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
fYear :
2013
Firstpage :
1214
Lastpage :
1219
Abstract :
To find the failure propagation mechanism from the complex electromechanical system of aircraft engine, this paper used the topological structure to describe the coupling relations, discussing the role of topological geometry method in the failure propagation. The topological structure statistical properties of the system were analyzed with small world net theory??and a failure propagation model based on the small world clustering was proposed, and the failure propagation paths and relevant key nodes with high pervasion ability were found with the Dijkstra algorithm. The results verify that this method can effectively find the weak point in the system, and provide an important basis for design improvements and failure prevention.
Keywords :
electromechanical actuators; engines; failure analysis; parallel algorithms; pattern clustering; Dijkstra algorithm; aircraft engine system; design improvements; electromechanical system; failure prevention; failure propagation analysis; small world clustering; small-world net model; topological geometry method; topological structure; Aircraft propulsion; Analytical models; Atmospheric modeling; Educational institutions; Electronic mail; Pain; Principal component analysis; Aircraft Engine System; Highest Risk Path of Failure Propagation; Intensity of Failure Propagation; Parameter of Network Topological Structure; Small-World Net Model;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2013 32nd Chinese
Conference_Location :
Xi´an
Type :
conf
Filename :
6639612
Link To Document :
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